Lunar missions benefit from varying the launch azimuth as a function of launch time to allow longer launch windows with minimum performance impacts. This variable azimuth approach allows the vehicle to track the Moon’s apparent motion due to Earth’s rotation. The Space Launch System (SLS) Block 1 vehicle design requires the mission to launch into an elliptical parking orbit to provide sufficient energy to insert Orion into a Trans-Lunar Injection (TLI) orbit. The primary benefit of varying the launch azimuth, and as a result the achieved orbit inclination, allows the SLS Interim Cryogenic Propulsion Stage (ICPS) to perform its TLI burn closer to perigee and take advantage of performing a burn in a location where the burn will optimally raise apogee.
Space Launch System Launch Windows and Day of Launch Processes
AAS/AIAA Astrodynamics Specialists Conference (Video presentation and paper submittal) ; 2020 ; Virtual, US
Conference paper
No indication
English
Space Launch System: Progress Towards Launch
NTIS | 2016
|Space Launch System: Progress Towards Launch
NTRS | 2016
|